Phenomenon Update: Look for Record Attempt in Summer 2011
#21
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Joined: Jan 2010
Posts: 59
Likes: 38
Are you sure? The current placement of the canard may cause dynamic instability and potential pilot induced oscillations (if there is direct linkage in the control of the canard wing). I’d certainly like to see the wind tunnel data before I got anywhere near 200 knots.
ND1
ND1
#23
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Joined: Jan 2010
Posts: 59
Likes: 38
I thought I spied some type of pivot mechanism in one of the pictures but you may be right (in which case there’s no risk of a PIO event). However the dynamic stability issue may yet be a concern with the canard’s current location. Can anyone familiar with the project confirm if the incidence of the canard is indeed adjustable and if so by what means?
Thanks,
ND1
Thanks,
ND1
#24
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Joined: May 2009
Posts: 538
Likes: 33
From: Greenville, North Carolina
I thought I spied some type of pivot mechanism in one of the pictures but you may be right (in which case there’s no risk of a PIO event). However the dynamic stability issue may yet be a concern with the canard’s current location. Can anyone familiar with the project confirm if the incidence of the canard is indeed adjustable and if so by what means?
Thanks,
ND1
Thanks,
ND1
#25
It was my understanding it was gyro/computer controlled ...
All images can be found here:
Exclusive Photos of Phenomenon by Sharkey-Images
All images can be found here:
Exclusive Photos of Phenomenon by Sharkey-Images
Last edited by SHARKEY-IMAGES; 12-10-2010 at 03:06 PM.
#26
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Joined: Apr 2001
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From: Beautiful Fort Lauderdale www.cheetahcat.com
My cunards were cockpit adjustable and work well being that far foreward they have a good mechanical advantage,What I can't figure out is why the fairing in of the tunnel/cockpit was done in that manner, there is a better way of doing that.
#28
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From: Boca/Brentwood
#29
I believe that is III.
#30
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Joined: Jul 2008
Posts: 730
Likes: 1
From: Darwin, Australia
I believe Al Copeland Jr confirmed in an interview(?) or article that the canard wing was controlled via computer which sensed lift weight at the front and adjusted angle to either increase or decrease according to speed. If it was all automated via computer, it would be a fantastic trim wing! I can't wait to see thing thing at full speed, it will be a sight to behold.
I for one, hope they can achieve what they have set out to do.
I for one, hope they can achieve what they have set out to do.



